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An Investigation Of The Effect Of A Tangential Gas Velocity On Combustion Instability
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Book Synopsis An Investigation of the Effect of a Tangential Gas Velocity on Combustion Instability by :
Download or read book An Investigation of the Effect of a Tangential Gas Velocity on Combustion Instability written by and published by . This book was released on 1969 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: A small, uncooled research rocket motor was built to study the effects of a vortex flow on combustion instability. Normal heptane and air were used as propellants with the air being divided into two flows; a primary flow at the center of the combustion chamber and a secondary flow at the periphery of the chamber. The secondary air provided the swirl which could be directed clockwise or counterclockwise at various angles or a straight mode of operation. Runs were made at various flow rates with the direction of swirl changed during the run. A first tangential high frequency mode of combustion instability was developed and a significant change in stability conditions was found when a vortex flow as generated within the combustion chamber. It was found that a swirl in one direction tended to decrease the instability while a flow in the opposite direction increased it. (Author).
Book Synopsis An Investigation of the Effect of a Tangential Gas Velocity on Combustion Instability by : Joseph Alan Kiel
Download or read book An Investigation of the Effect of a Tangential Gas Velocity on Combustion Instability written by Joseph Alan Kiel and published by . This book was released on 1969 with total page 75 pages. Available in PDF, EPUB and Kindle. Book excerpt: A small, uncooled research rocket motor was built to study the effects of a vortex flow on combustion instability. Normal heptane and air were used as propellants with the air being divided into two flows; a primary flow at the center of the combustion chamber and a secondary flow at the periphery of the chamber. The secondary air provided the swirl which could be directed clockwise or counterclockwise at various angles or a straight mode of operation. Runs were made at various flow rates with the direction of swirl changed during the run. A first tangential high frequency mode of combustion instability was developed and a significant change in stability conditions was found when a vortex flow as generated within the combustion chamber. It was found that a swirl in one direction tended to decrease the instability while a flow in the opposite direction increased it. (Author).
Book Synopsis Evaluation of Tangential Velocity Effects on Spinning Transverse Combustion Instability by : Marcus F. Heidmann
Download or read book Evaluation of Tangential Velocity Effects on Spinning Transverse Combustion Instability written by Marcus F. Heidmann and published by . This book was released on 1966 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Effect of Tangential Gas Velocity on Combustion Instability in a Liquid-Gas Combustor by : Donald William Avery (Jr.)
Download or read book The Effect of Tangential Gas Velocity on Combustion Instability in a Liquid-Gas Combustor written by Donald William Avery (Jr.) and published by . This book was released on 1971 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt: A small, uncooled liquid rocket motor was utilized to examine the effects of the magnitude and direction of a steady vortex velocity on combustion instability. The rocket operated on normal heptane and air, with air flow rates controllable to allow for various amounts of tangential momentum. Results of the investigation indicated that an energy feedback mechanism, through tangential momentum, did exist for both tangential and radial modes of instability. It was further shown that limit values of tangential velocity did exist, for a particular combustor, above and below which instability did not occur. (Author).
Book Synopsis Measured Effects of Gaseous Flow System Dynamics on Acoustic-mode Combustion Instability by : John Frederick Groeneweg
Download or read book Measured Effects of Gaseous Flow System Dynamics on Acoustic-mode Combustion Instability written by John Frederick Groeneweg and published by . This book was released on 1969 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Combustion Instability Limits Determined by a Nonlinear Theory and a One-dimensional Model by : Richard J. Priem
Download or read book Combustion Instability Limits Determined by a Nonlinear Theory and a One-dimensional Model written by Richard J. Priem and published by . This book was released on 1962 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :Miron Semenovich Natanzon Publisher :AIAA (American Institute of Aeronautics & Astronautics) ISBN 13 : Total Pages :298 pages Book Rating :4.F/5 ( download)
Book Synopsis Combustion Instability by : Miron Semenovich Natanzon
Download or read book Combustion Instability written by Miron Semenovich Natanzon and published by AIAA (American Institute of Aeronautics & Astronautics). This book was released on 1999 with total page 298 pages. Available in PDF, EPUB and Kindle. Book excerpt: First published in 1986 by Mashinostroenie, Moscow.
Book Synopsis Detonation and Two-Phase Flow by : S Penner
Download or read book Detonation and Two-Phase Flow written by S Penner and published by Elsevier. This book was released on 2012-12-02 with total page 381 pages. Available in PDF, EPUB and Kindle. Book excerpt: Progress in Astronautics and Rocketry, Volume 6: Detonation and Two-Phase Flow compiles technical papers presented at the ARS Propellants, Combustion, and Liquid Rockets Conference held in Palm Beach, Florida on April 26-28, 1961. This book provides an excellent illustration of research and development on a selected group of problems relating to detonations, two-phase nozzle flow, and combustion in liquid fuel rocket engines. This volume is divided into two parts. Part 1 covers the entire range of physical conditions under which detonation may be initiated or sustained, such as high explosives, solid propellants, liquid sprays, and gases. Experimental and theoretical studies are also discussed, including the significant progress of the basic phenomena involved in transition from deflagration to detonation, and nature of stable detonations in dilute sprays and other systems. The perennial problems associated with high frequency instabilities in liquid fuel rocket engines are considered in Part 2. This publication is valuable to students and investigators working in the field of propulsion research and development.
Book Synopsis An Experimental Investigation of Velocity Coupling in Combustion Instability by : Y. Ma
Download or read book An Experimental Investigation of Velocity Coupling in Combustion Instability written by Y. Ma and published by . This book was released on 1990 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Stability Limits and Efficiency of Swirl-can Combustor Modules Burning Natural Gas Fuel by : Nicholas R. Marchionna
Download or read book Stability Limits and Efficiency of Swirl-can Combustor Modules Burning Natural Gas Fuel written by Nicholas R. Marchionna and published by . This book was released on 1970 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Calculations of Combustion Response Profiles and Oscillations by :
Download or read book Calculations of Combustion Response Profiles and Oscillations written by and published by . This book was released on 1993 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Systematic Investigation of Bluff-Body Combustion Instability by :
Download or read book Systematic Investigation of Bluff-Body Combustion Instability written by and published by . This book was released on 2005 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt: The objectives, work carried out and results obtained during a Phase 11 STTR project are reported. An capability for unsteady flows is added to a sensitivity tool which numerically solves the continuous sensitivity equations. A feedback control law is implemented to control numerically an acoustic instability, which is modeled by coupling pressure and velocity perturbations at an inflow boundary condition. Axi-symmetric simulations are presented for the burner both without methane injection and with five injection locations. The computation is performed using a 12-specie methane/air chemistry model with finite-rate chemical kinetics. An experimental investigation is pursued of a circular bluff-body burner equipped with multiple fuel injectors. The axial injector is used as a pilot flame for premixed observations at equivalence ratios of 0.4 and 0.5.
Book Synopsis Solid Propellant Rocket Research by : Martin Summerfield
Download or read book Solid Propellant Rocket Research written by Martin Summerfield and published by Elsevier. This book was released on 2013-11-11 with total page 713 pages. Available in PDF, EPUB and Kindle. Book excerpt: Solid Propellant Rocket Research
Book Synopsis Abstracts of Dissertations, Theses and Research Papers Submitted by Candidates for Degrees by : Naval Postgraduate School (U.S.)
Download or read book Abstracts of Dissertations, Theses and Research Papers Submitted by Candidates for Degrees written by Naval Postgraduate School (U.S.) and published by . This book was released on 1966 with total page 628 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Compilation of Abstracts of Dissertations, Theses and Research Papers Submitted by Candidates for Degrees by : Naval Postgraduate School (U.S.)
Download or read book Compilation of Abstracts of Dissertations, Theses and Research Papers Submitted by Candidates for Degrees written by Naval Postgraduate School (U.S.) and published by . This book was released on 1971 with total page 408 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :United States. National Aeronautics and Space Administration Scientific and Technical Information Division Publisher : ISBN 13 : Total Pages :2300 pages Book Rating :4.F/5 ( download)
Book Synopsis NASA Scientific and Technical Reports by : United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Download or read book NASA Scientific and Technical Reports written by United States. National Aeronautics and Space Administration Scientific and Technical Information Division and published by . This book was released on 1967 with total page 2300 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 704 pages. Available in PDF, EPUB and Kindle. Book excerpt:
